************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file (leparagliding 3.20V) * ************************************************************** * Date: 2022-09-21 ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "Laboratori d'envol" * Wing name "gnuReflex-test" * Drawing scale 1.0 * Wing scale 0.861602042 * Number of cells 53 * Number of ribs 54 * Alpha wingtip, parameter, (alpha center) 5.5 1 0.0 * Paraglider type and parameter "ds" 1 * Rib geometric parameters * Rib x-rib y-LE y-TE xp z beta RP Washin z_rot z_pos 1 0.00 -0.00 254.49 0.00 0.00 0.00 33.33 0.00 0.00 50. 2 24.79 0.16 254.42 24.79 0.45 2.08 33.33 0.00 0.22 50. 3 49.55 0.65 254.20 49.50 1.79 4.09 33.33 0.00 0.43 50. 4 74.25 1.45 253.84 74.10 4.02 6.25 33.33 0.00 0.65 50. 5 98.87 2.58 253.34 98.52 7.12 8.26 33.33 0.00 0.86 50. 6 123.39 4.04 252.70 122.72 11.08 10.27 33.33 0.00 1.07 50. 7 147.78 5.82 251.91 146.64 15.87 12.43 33.33 0.00 1.29 50. 8 172.02 7.93 250.98 170.22 21.48 14.53 33.33 0.00 1.50 50. 9 196.10 10.37 249.91 193.38 28.06 17.22 33.33 0.00 1.78 50. 10 219.98 13.14 248.70 216.00 35.70 20.13 33.33 0.00 2.06 50. 11 243.64 16.26 247.34 238.02 44.34 22.82 33.33 0.00 2.33 50. 12 267.06 19.72 245.84 259.38 53.94 25.51 33.33 0.00 2.58 50. 13 290.21 23.53 244.20 280.03 64.41 28.20 33.33 0.00 2.84 50. 14 313.07 27.73 242.41 299.91 75.70 30.90 33.33 0.00 3.08 50. 15 335.61 32.60 240.49 318.96 87.73 33.59 33.33 0.00 3.32 50. 16 357.76 38.20 238.42 337.10 100.45 36.81 33.33 0.00 3.60 50. 17 379.51 44.53 236.22 354.04 114.07 40.77 33.33 0.00 3.92 50. 18 400.79 51.56 233.89 369.72 128.46 44.49 33.33 0.00 4.21 50. 19 421.58 59.30 231.42 384.09 143.47 48.00 33.33 0.00 4.46 50. 20 441.83 67.73 228.82 397.14 158.95 51.73 33.33 0.00 4.71 50. 21 461.50 76.85 226.11 408.88 174.74 55.02 33.33 0.00 4.92 50. 22 480.56 86.67 223.27 419.29 190.70 58.85 33.33 0.00 5.14 50. 23 498.96 97.20 220.27 428.28 206.75 62.61 33.33 0.00 5.33 50. 24 516.65 108.47 217.08 435.89 222.72 66.38 33.33 0.00 5.50 50. 25 533.60 120.56 213.72 442.19 238.44 69.93 33.33 0.00 5.64 50. 26 549.73 133.57 210.22 447.28 253.75 73.27 33.33 0.00 5.75 50. 27 565.00 147.75 206.60 451.94 271.43 76.41 33.33 0.00 5.84 50. ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name, intake in, intake out, open, disp, rrw 1 rcandidate1.txt 1.60 6.30 1 0 1 0 2 rcandidate1.txt 1.60 6.30 1 0 1 15 3 rcandidate1.txt 1.60 6.30 1 0 1 15 4 rcandidate1.txt 1.60 6.30 1 0 1 15 5 rcandidate1.txt 1.60 6.30 1 0 1 15 6 rcandidate1.txt 1.60 6.30 1 0 1 15 7 rcandidate1.txt 1.60 6.30 1 0 1 15 8 rcandidate1.txt 1.60 6.30 1 0 1 15 9 rcandidate1.txt 1.60 6.30 1 0 1 15 10 rcandidate1.txt 1.60 6.30 1 0 1 15 11 rcandidate1.txt 1.60 6.30 1 0 1 15 12 rcandidate1.txt 1.60 6.30 1 0 1 15 13 rcandidate1.txt 1.60 6.30 1 0 1 15 14 rcandidate1.txt 1.60 6.30 1 0 1 15 15 rcandidate1.txt 1.60 6.30 1 0 1 15 16 rcandidate1.txt 1.60 6.30 1 0 1 15 17 rcandidate1.txt 1.60 6.30 1 0 1 15 18 rcandidate1.txt 1.60 6.30 1 0 1 15 19 rcandidate1.txt 1.60 6.30 1 0 1 15 20 rcandidate1.txt 1.60 6.30 1 0 1 15 21 rcandidate1.txt 1.60 6.30 1 0 1 15 22 rcandidate1.txt 1.60 6.30 1 0 1 15 23 rcandidate1.txt 1.60 6.30 1 1 1 15 24 rcandidate1.txt 1.60 6.30 1 1 1 15 25 rcandidate1.txt 1.60 6.30 1 1 1 15 26 rcandidate1.txt 1.60 6.30 1 1 1 15 27 rcandidate1.txt 1.60 6.30 1 1 1 0 ************************************************************* * 3. ANCHOR POINTS * ************************************************************* * Airf Anch A B C D E F 1 0 12.0 40.0 68.0 81.0 85.00 100 2 4 12.0 40.0 68.0 81.0 85.00 100 3 4 12.0 40.0 68.0 81.0 85.00 95 4 4 12.0 40.0 68.0 81.0 85.00 95 5 4 12.0 40.0 68.0 81.0 85.00 100 6 4 12.0 40.0 68.0 81.0 85.00 95 7 0 12.0 40.0 68.0 81.0 0.0 100 8 0 12.0 40.0 68.0 81.0 0.0 100 9 3 12.0 40.0 68.0 81.0 0.0 95 10 3 12.0 40.0 68.0 81.0 0.0 100 11 0 12.0 40.0 68.0 81.0 0.0 100 12 3 12.0 40.0 68.0 81.0 0.0 95 13 3 12.0 40.0 68.0 81.0 0.0 100 14 0 12.0 40.0 68.0 81.0 0.0 100 15 0 12.0 40.0 68.0 81.0 0.0 95 16 3 12.0 40.0 68.0 81.0 0.0 100 17 3 12.0 40.0 68.0 81.0 0.0 100 18 0 12.0 40.0 68.0 81.0 0.0 95 19 3 12.0 40.0 68.0 81.0 0.0 100 20 3 12.0 40.0 68.0 81.0 0.0 95 21 0 12.0 40.0 68.0 81.0 0.0 100 22 3 12.0 40.0 68.0 81.0 0.0 93 23 3 12.0 40.0 68.0 81.0 0.0 100 24 0 12.0 40.0 68.0 81.0 0.0 93 25 3 12.0 40.0 68.0 81.0 0.0 93 26 0 12.0 40.0 68.0 81.0 0.0 100 27 2 5. 55 66 95 0 100 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 1 19 19 6 1 5.6772 1.2020 2.55 2.55 0. 0. 0. 1 19.1340 3.1953 5.17 5.17 0. 0. 0. 1 34.9116 3.7191 4.30 4.30 0. 0. 0. 1 48.5396 3.2010 3.38 3.38 0. 0. 0. 1 60.3734 2.6921 2.45 2.45 0. 0. 0. 1 71.3037 2.2690 1.75 1.75 0. 0. 0. ************************************************************* * 5. SKIN TENSION * ************************************************************* Extrados Intrados 0. 0. 0. 0. 7.5 1.3 10. 1.33 15. 2.8 20. 2.8 80. 2.8 80. 2.8 90. 1.33 90. 1.33 100. 0.0 100. 0. 0.0001 1000 1.0 ************************************************************* * 6. SEWING ALLOWANCES * ************************************************************* 15 25 25 upper panels (mm) 15 25 25 lower panels (mm) 15 ribs (mm) 15 vribs (mm) ************************************************************* * 7. MARKS ************************************************************* 25 0.03 0.135 ************************************************************ * 8. Global angle of attack estimation * ************************************************************* * Finesse GR 8.8 * Plumb point % of chord 33.7 * Calage % 45 * Risers lenght cm 50 * Line lenght cm 655 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 0 3 14 4 1 1 2 1 3 1 4 1 1 2 - 1 2 3 4 4 1 1 2 1 3 1 4 2 1 3 - 1 2 3 4 4 1 1 2 1 3 2 4 3 1 5 - 1 2 3 4 4 1 1 2 1 3 2 4 4 1 6 - 1 2 3 4 4 1 1 2 2 3 3 4 5 1 9 - 1 2 3 4 4 1 1 2 2 3 3 4 6 1 10 - 1 2 3 4 4 1 1 2 2 3 4 4 7 1 12 - 1 2 3 4 4 1 1 2 2 3 4 4 8 1 13 - 1 2 3 4 4 1 1 2 3 3 5 4 9 1 16 - 1 2 3 4 4 1 1 2 3 3 5 4 10 1 17 - 1 2 3 4 4 1 1 2 3 3 6 4 11 1 19 - 1 2 3 4 4 1 1 2 3 3 6 4 12 1 20 - 1 2 3 4 4 1 1 2 3 3 7 4 13 1 22 - 1 2 3 4 4 1 1 2 3 3 7 4 14 1 23 - 1 2 3 4 19 4 1 1 2 1 3 1 4 1 2 2 - 1 2 3 4 4 1 1 2 1 3 1 4 2 2 3 - 1 2 3 4 4 1 1 2 1 3 2 4 3 2 5 - 1 2 3 4 4 1 1 2 1 3 2 4 4 2 6 - 1 2 3 4 4 1 1 2 2 3 3 4 5 2 9 - 1 2 3 4 4 1 1 2 2 3 3 4 6 2 10 - 1 2 3 4 4 1 1 2 2 3 4 4 7 2 12 - 1 2 3 4 4 1 1 2 2 3 4 4 8 2 13 - 1 2 3 4 4 1 1 2 3 3 5 4 9 2 16 - 1 2 3 4 4 1 1 2 3 3 5 4 10 2 17 - 1 2 3 4 4 1 1 2 3 3 6 4 11 2 19 - 1 2 3 4 4 1 1 2 3 3 6 4 12 2 20 - 1 2 3 4 4 1 1 2 3 3 7 4 13 2 22 - 1 2 3 4 4 1 1 2 3 3 7 4 14 2 23 - 1 2 3 4 4 1 1 2 4 3 8 4 15 1 25 - 1 2 3 4 4 1 1 2 4 3 8 4 16 2 25 - 1 2 3 4 3 1 1 2 4 3 9 0 0 3 25 - 1 2 3 4 4 1 1 2 4 3 10 4 17 1 27 - 1 2 3 4 4 1 1 2 4 3 10 4 18 2 27 - 1 2 3 4 18 4 1 1 2 1 3 1 4 1 3 2 - 1 2 3 4 4 1 1 2 1 3 1 4 2 3 3 - 1 2 3 4 4 1 1 2 1 3 1 4 3 4 2 - 1 2 3 4 4 1 1 2 1 3 1 4 4 4 3 - 1 2 3 4 4 1 1 2 1 3 2 4 5 3 5 - 1 2 3 4 4 1 1 2 1 3 2 4 6 3 6 - 1 2 3 4 4 1 1 2 1 3 2 4 7 4 5 - 1 2 3 4 4 1 1 2 1 3 2 4 8 4 6 - 1 2 3 4 4 1 1 2 2 3 3 4 9 3 9 - 1 2 3 4 4 1 1 2 2 3 3 4 10 3 10 - 1 2 3 4 4 1 1 2 2 3 4 4 11 3 12 - 1 2 3 4 4 1 1 2 2 3 4 4 12 3 13 - 1 2 3 4 4 1 1 2 3 3 5 4 13 3 16 - 1 2 3 4 4 1 1 2 3 3 5 4 14 3 17 - 1 2 3 4 4 1 1 2 3 3 6 4 15 3 19 - 1 2 3 4 4 1 1 2 3 3 6 4 16 3 20 - 1 2 3 4 4 1 1 2 3 3 7 4 17 3 22 - 1 2 3 4 4 1 1 2 3 3 7 4 18 3 23 - 1 2 3 4 *************************************************** * 10. BRAKES *************************************************** 230 10 3 1 1 2 1 3 1 0 0 6 3 - 6 2 4 3 1 1 2 1 3 2 0 0 6 6 - 6 2 4 4 1 1 2 2 3 3 4 1 6 9 - 6 2 3 4 4 1 1 2 2 3 3 4 2 6 11 - 6 2 3 4 4 1 1 2 2 3 4 4 3 6 15 - 6 2 3 4 4 1 1 2 2 3 4 4 4 6 18 - 6 2 3 4 4 1 1 2 3 3 5 4 5 6 20 - 6 2 3 4 4 1 1 2 3 3 5 4 6 6 22 - 6 2 3 4 4 1 1 2 3 3 6 4 7 6 24 - 6 2 3 4 4 1 1 2 3 3 6 4 8 6 26 - 6 2 3 4 * Brake distribution 0 25 55 70 100 0 0 0 0 0 *************************************************** * 11. Ramification lengths *************************************************** 3 150 4 250 100 3 160 4 250 100 *************************************************** * 12. H V and VH ribs *************************************************** 149 80 150 1 1 1 1 2 1 2.5 0 0 0 2 1 2 1 3 1 2.5 0 0 0 3 1 3 1 4 1 2.5 0 0 0 4 1 4 1 5 1 2.5 0 0 0 5 1 5 1 6 1 2.5 0 0 0 6 1 6 1 7 1 2.5 0 0 0 7 1 7 1 8 1 2.5 0 0 0 8 1 8 1 9 1 2.5 0 0 0 9 1 9 1 10 1 2.5 0 0 0 10 1 10 1 11 1 2.5 0 0 0 11 1 11 1 12 1 2.5 0 0 0 12 1 12 1 13 1 2.5 0 0 0 13 1 13 1 14 1 2.5 0 0 0 14 1 14 1 15 1 2.5 0 0 0 15 1 15 1 16 1 2.5 0 0 0 16 1 16 1 17 1 2.5 0 0 0 17 1 17 1 18 1 2.5 0 0 0 18 1 18 1 19 1 2.5 0 0 0 19 1 19 1 20 1 2.5 0 0 0 20 1 20 1 21 1 2.5 0 0 0 21 1 21 1 22 1 2.0 0 0 0 22 1 22 1 23 1 2.0 0 0 0 23 1 23 1 24 1 2.0 0 0 0 24 1 24 1 25 1 2.0 0 0 0 26 1 1 2 2 2 2.5 0 0 0 27 1 2 2 3 2 2.5 0 0 0 28 1 3 2 4 2 2.5 0 0 0 29 1 4 2 5 2 2.5 0 0 0 30 1 5 2 6 2 2.5 0 0 0 31 1 6 2 7 2 2.5 0 0 0 32 1 7 2 8 2 2.5 0 0 0 33 1 8 2 9 2 2.5 0 0 0 34 1 9 2 10 2 2.5 0 0 0 35 1 10 2 11 2 2.5 0 0 0 36 1 11 2 12 2 2.5 0 0 0 37 1 12 2 13 2 2.5 0 0 0 38 1 13 2 14 2 2.5 0 0 0 39 1 14 2 15 2 2.5 0 0 0 40 1 15 2 16 2 2.5 0 0 0 41 1 16 2 17 2 2.5 0 0 0 42 1 17 2 18 2 2.5 0 0 0 43 1 18 2 19 2 2.5 0 0 0 44 1 19 2 20 2 2.5 0 0 0 45 1 20 2 21 2 2.5 0 0 0 46 1 21 2 22 2 2.0 0 0 0 47 1 22 2 23 2 2.0 0 0 0 48 1 23 2 24 2 2.0 0 0 0 49 1 24 2 25 2 2.0 0 0 0 51 1 1 3 2 3 2.5 0 0 0 52 1 2 3 3 3 2.5 0 0 0 53 1 3 3 4 3 2.5 0 0 0 54 1 4 3 5 3 2.5 0 0 0 55 1 5 3 6 3 2.5 0 0 0 56 1 6 3 7 3 2.5 0 0 0 57 1 7 3 8 3 2.5 0 0 0 58 1 8 3 9 3 2.5 0 0 0 59 1 9 3 10 3 2.5 0 0 0 60 1 10 3 11 3 2.5 0 0 0 61 1 11 3 12 3 2.5 0 0 0 62 1 12 3 13 3 2.5 0 0 0 63 1 13 3 14 3 2.5 0 0 0 64 1 14 3 15 3 2.5 0 0 0 65 1 15 3 16 3 2.5 0 0 0 66 1 16 3 17 3 2.5 0 0 0 67 1 17 3 18 3 2.5 0 0 0 68 1 18 3 19 3 2.5 0 0 0 69 1 19 3 20 3 2.5 0 0 0 70 1 20 3 21 3 2.5 0 0 0 71 1 21 3 22 3 2.0 0 0 0 72 1 22 3 23 3 2.0 0 0 0 73 1 23 3 24 3 2.0 0 0 0 72 1 24 3 25 3 2.0 0 0 0 73 16 1 81. 0. 1.5 1.5 2 81. 0. 1.5 1.5 74 16 2 81. 0. 1.5 1.5 3 81. 0. 1.5 1.5 75 16 3 81. 0. 1.5 1.5 4 81. 0. 1.5 1.5 76 16 4 81. 0. 1.5 1.5 5 81. 0. 1.5 1.5 77 16 5 81. 0. 1.5 1.5 6 81. 0. 1.5 1.5 78 16 6 81. 0. 1.5 1.5 7 81. 0. 1.5 1.5 79 16 7 81. 0. 1.5 1.5 8 81. 0. 1.5 1.5 80 16 8 81. 0. 1.5 1.5 9 81. 0. 1.5 1.5 81 16 9 81. 0. 1.5 1.5 10 81. 0. 1.5 1.5 82 16 10 81. 0. 1.5 1.5 11 81. 0. 1.5 1.5 83 16 11 81. 0. 1.5 1.5 12 81. 0. 1.5 1.5 84 16 12 81. 0. 1.5 1.5 13 81. 0. 1.5 1.5 85 16 13 81. 0. 1.5 1.5 14 81. 0. 1.5 1.5 86 16 14 81. 0. 1.5 1.5 15 81. 0. 1.5 1.5 87 16 15 81. 0. 1.5 1.5 16 81. 0. 1.5 1.5 88 16 16 81. 0. 1.5 1.5 17 81. 0. 1.5 1.5 89 16 17 81. 0. 1.5 1.5 18 80. 0. 1.5 1.5 90 16 18 80. 0. 1.5 1.5 19 78. 0. 1.5 1.5 91 16 19 78. 0. 1.5 1.5 20 76. 0. 1.5 1.5 92 16 20 76. 0. 1.5 1.5 21 74. 0. 1.5 1.5 93 16 21 74. 0. 1.5 1.5 22 72. 0. 1.5 1.5 94 16 22 72. 0. 1.5 1.5 23 70. 0. 1.5 1.5 95 16 23 70. 0. 1.5 1.5 24 68. 0. 1.5 1.5 96 16 1 12. 100. 10.0 10.0 2 12. 0. 1.6 1.6 97 16 3 12. 0. 1.6 1.6 4 12. 100. 10.0 10.0 98 16 4 12. 100. 10.0 10.0 5 12. 0. 1.6 1.6 99 16 6 12. 0. 1.6 1.6 7 12. 100. 10.0 10.0 100 16 7 12. 100. 10.0 10.0 8 12. 100. 10.0 10.0 101 16 8 12. 100. 10.0 10.0 9 12. 0. 1.6 1.6 102 16 10 12. 0. 1.6 1.6 11 12. 100. 10.0 10.0 103 16 11 12. 100. 8.0 10.0 12 12. 0. 1.6 1.6 104 16 13 12. 0. 1.6 1.6 14 12. 100. 10.0 10.0 105 16 14 12. 100. 10.0 10.0 15 12. 100. 10.0 10.0 106 16 15 12. 100. 10.0 10.0 16 12. 0. 1.6 1.6 107 16 17 12. 0. 1.6 1.6 18 12. 100. 10.0 10.0 108 16 18 12. 100. 8.0 10.0 19 12. 0. 1.6 1.6 109 16 20 12. 0. 1.6 1.6 21 12. 100. 10.0 10.0 110 16 21 12. 100. 8.0 10.0 22 12. 0. 1.6 1.6 111 16 23 12. 0. 1.6 1.6 24 12. 100. 10.0 10.0 112 16 24 12. 100. 8.0 10.0 25 12. 0. 1.6 1.6 113 16 1 40. 100. 10.0 10.0 2 40. 0. 1.6 1.6 114 16 3 40. 0. 1.6 1.6 4 40. 100. 10.0 10.0 115 16 4 40. 100. 10.0 10.0 5 40. 0. 1.6 1.6 116 16 6 40. 0. 1.6 1.6 7 40. 100. 10.0 10.0 117 16 7 40. 100. 10.0 10.0 8 40. 100. 10.0 10.0 118 16 8 40. 100. 10.0 10.0 9 40. 0. 1.6 1.6 119 16 10 40. 0. 1.6 1.6 11 40. 100. 10.0 10.0 120 16 11 40. 100. 8.0 10.0 12 40. 0. 1.6 1.6 121 16 13 40. 0. 1.6 1.6 14 40. 100. 10.0 10.0 122 16 14 40. 100. 10.0 10.0 15 40. 100. 10.0 10.0 123 16 15 40. 100. 10.0 10.0 16 40. 0. 1.6 1.6 124 16 17 40. 0. 1.6 1.6 18 40. 100. 10.0 10.0 125 16 18 40. 100. 8.0 10.0 19 40. 0. 1.6 1.6 126 16 20 40. 0. 1.6 1.6 21 40. 100. 10.0 10.0 127 16 21 40. 100. 8.0 10.0 22 40. 0. 1.6 1.6 128 16 23 40. 0. 1.6 1.6 24 40. 100. 10.0 10.0 129 16 24 40. 100. 8.0 10.0 25 40. 0. 1.6 1.6 130 16 1 68. 100. 10.0 6.0 2 68. 0. 1.6 1.6 131 16 3 68. 0. 1.6 1.6 4 68. 100. 10.0 6.0 132 16 4 68. 100. 10.0 6.0 5 68. 0. 1.6 1.6 133 16 6 68. 0. 1.6 1.6 7 68. 100. 10.0 10.0 134 16 7 68. 100. 10.0 10.0 8 68. 100. 10.0 10.0 135 16 8 68. 100. 10.0 10.0 9 68. 0. 1.6 1.6 136 16 10 68. 0. 1.6 1.6 11 68. 100. 10.0 10.0 137 16 11 68. 100. 8.0 10.0 12 68. 0. 1.6 1.6 138 16 13 68. 0. 1.6 1.6 14 68. 100. 10.0 10.0 139 16 14 68. 100. 10.0 10.0 15 68. 100. 10.0 10.0 140 16 15 68. 100. 10.0 10.0 16 68. 0. 1.6 1.6 141 16 17 68. 0. 1.6 1.6 18 68. 100. 10.0 10.0 142 16 18 68. 100. 8.0 10.0 19 68. 0. 1.6 1.6 143 16 20 68. 0. 1.6 1.6 21 68. 100. 10.0 10.0 144 16 21 68. 100. 8.0 10.0 22 68. 0. 1.6 1.6 145 16 23 68. 0. 1.6 1.6 24 68. 100. 10.0 10.0 146 16 24 68. 100. 8.0 10.0 25 68. 0. 1.6 1.6 147 16 1 81. 100. 6.0 10.0 2 81. 0. 1.6 1.6 148 16 3 81. 0. 1.6 1.6 4 81. 100. 6.0 10.0 149 16 4 81. 100. 6.0 10.0 5 81. 0. 1.6 1.6 ***************************************************** * 15. Extrados colors ***************************************************** 1 1 1 1 0. 0. ***************************************************** * 16. Intrados colors ***************************************************** 0 ***************************************************** * 17. Aditional rib points ***************************************************** 0 ***************************************************** * 18. Elastic lines corrections ***************************************************** 180 75 25 40 40 20 35 35 20 10 35 35 15 10 5 1 0.08 0.2 0.2 2 0.08 0.2 0.2 3 0.08 0.2 0.2 4 0.08 0.2 0.2 5 0.08 0.2 0.2 ****************************************************** * 19. DXF layer names ****************************************************** 10 general default line-external cutexternal line-sewing cutinternal points points circles circles triangles triangle square square text text reference refer notes notes ****************************************************** * 20. Marks types ****************************************************** 10 typepoint 1 0.25 1.2 2 0.3 1.2 typepoint2 1 0.25 1.2 2 0.2 1.2 typepoint3 1 0.25 1.2 2 0.2 1.2 typevent 1 10. 0.0 2 2.0 0.0 typetab 1 10. 0.0 3 2.0 0.0 typejonc 1 10. 0.0 2 2.0 0.0 typeref 1 5.0 1. 1 2.0 0.0 type8 1 0.2 5.0 1 0.0 5.0 type9 1 0.0 7.0 1 3.2 4.5 type10 1 0.0 6.0 1 0.0 3.33 ******************************************************* * 21. JONCS DEFINITION (NYLON RODS) ******************************************************* 1 2 1 1 24 5.5 10. 1.5 2.0 5. 14. 2.2 2.0 0.0 9.35 6.3 9.35 2 18 20 5. 9. 2.5 2.0 5. 14. 3. 2.0 0.0 9.35 6.3 9.35 ******************************************************* * 22. NOSE MYLARS DEFINITION ******************************************************* 0 ******************************************************* * 23. TAB REINFORCEMENTS ******************************************************* 0 ******************************************************* * 24. GENERAL 2D DXF OPTIONS ******************************************************* 1 A_lines_color 1 red B_lines_color 30 orange C_lines_color 3 green D_lines_color 4 cyan E_lines_color 6 magenta F_lines_color 5 blue ******************************************************* * 25. GENERAL 3D DXF OPTIONS ******************************************************* 1 A_lines_color 1 red B_lines_color 8 grey C_lines_color 8 grey D_lines_color 8 grey E_lines_color 8 grey F_lines_color 30 orange Extrados 1 5 blue Vents 0 1 red Intrados 0 3 green ******************************************************* * 26. GLUE VENTS ******************************************************* 1 1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0 9 0 10 0 11 0 12 0 13 0 14 0 15 0 16 0 17 0 18 0 19 0 20 0 21 0 22 0 23 -2 24 -1 25 -1 26 -1 27 -1 ******************************************************* * 27. SPECIAL WING TIP ******************************************************* 1 AngleLE 55. AngleTE 5. ******************************************************* * 28. PARAMETERS FOR CALAGE VARIATION ******************************************************* 1 4 10. 30.35 49.29 76.27 0 0 -3.0 10 5.0 20 ******************************************************* * 29. 3D SHAPING ******************************************************* 1 1 groups 1 group 1 1 27 upper 0 1 lower 0 1 * Print parameters Inter3D 0 1 26 1 Ovali3D 1 1 26 0 tesse3D 0 1 27 1 exteDXF 0 1 27 1 exteSTL 1 1 27 1 ******************************************************* * 30. AIRFOIL THICKNESS MODIFICATION ******************************************************* 1 1 1.0 2 1.0 3 1.0 4 1.0 5 1.0 6 1.0 7 1.0 8 1.0 9 1.0 10 1.0 11 1.0 12 1.0 13 1.0 14 1.0 15 1.0 16 1.0 17 1.0 18 1.0 19 1.0 20 1.0 21 1.0 22 1.0 23 1.0 24 1.0 25 1.0 26 1.0 27 0.4 ******************************************************* * 31. NEW SKIN TENSION MODULE ******************************************************* 1 1 * Skin tension group number "1" from rib 1 to 27, 14 points, type "1" 1 1 27 14 1 1 0. 0.03 0. 0. 2 5. 0.4 10. 0.625 3 10.0 1.0 20. 1.25 4 15. 1.94 30. 1.875 5 17.5 2.93 35 2.1875 6 20. 3.32 40. 2.5 7 25. 3.5 65. 2.5 8 50. 3.5 70. 2.4 9 55. 3.33 75. 2.3 10 65. 2.77 80. 2.0 11 70. 2.35 85. 1.5 12 90. 0.67 90. 0.9 13 95. 0.19 95. 0.3 14 100. 0.0 100. 0.03 ******************************************************* * 32. PARAMETERS FOR PARTS SEPARATION ******************************************************* 1 panel_x 1.2 panel_x_min 1.0 panel_y 0.8 rib_x 1.0 rib_y 1.0 rib_1y 1.8 parameter7 1.0 parameter8 1.0 parameter9 1.0 parameter10 1.0 ******************************************************* * 33. DETAILED RISERS ******************************************************* 1 1 A 50.0 cm B 65.0 cm C 80.0 cm ******************************************************* * 34. LINES CHARACTERISTICS TABLE ******************************************************* 1 6 1 c 5.0 Riser 1000 daN u_dyneem 10.0 g p 12. cm 7 2 c 1.90 Line275 275 daN s_dyneem 2.26 g s 12. cm 1 3 c 1.40 Line160 160 daN s_dyneem 1.34 g s 10. cm 3 4 c 1.15 Line120 120 daN s_dyneem 1.00 g s 10. cm 5 5 c 0.80 Line100U 100 daN u_dyneem 0.43 g p 8. cm 2 6 c 2.00 Line200B 200 daN s_dynemm 3.10 g s 12. cm 6 ******************************************************* * 35. SOLVE EQUILIBRIUM EQUATIONS ******************************************************* 1 g 9.807 m/s2 gravity of Earth ro 1.225 kg/m3 air mass density mu 18.46 muPa·s air dynamic viscosity (microPascals) V 12.4 m/s estimated flow speed Alpha 9.45 deg estimated wing angle of attact at trim speed Cl 0.67913 wing lift coefficient cle 1.0 lift correction coefficient Cd 0.03790 wing drag coefficient cde 1.1 drag correction coefficient Cm 0.0 wing moment coefficient Spilot 0.438 m2 pilot+harness frontal surface Cdpilot 0.6 pilot+harness drag coefficient Mw 4.0 kg wing mass Mp 70 kg pilot mass included harness and instruments Pmc 0.2 m pilot mass center below main karabiners Mql 8.0 g one quick link mass (riser-lines) Ycp 0.575 m y-coordinate center of pressure Zcp 0.395 m z-coordinate center of pressure ******************************************************* * 36. CREATE FILES FOR XFLR5 ANALYSIS ******************************************************* 1 * Panel parameters 10 chord nr 5 per cell 1 cosine distribution along chord 0 uniform along span * Include billowed airfoils (more accuracy) 0 ******************************************************* * 37. SOME SPECIAL PARAMETERS ******************************************************* 1 6 1291 8 nsegments in transverse direction (stl surfaces) 1341 0 use CAD colors for each line type according table 34 1146 36. gravity center in % of a typical section (default is 36%) 1351 1 Solve method (1 or 6) 1352 2 Use flat area (1) or projected area (2) 1353 2 Print normal (0) or advanced detailed output (1),(2)